Networked redundancy aircraft control system
Patent Information
- Authority / Receiving Office
- CN ยท China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- NAT UNIV OF DEFENSE TECH
- Publication Date
- 2020-07-24
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Figure 1
Abstract
Description
technical field
[0001] The invention belongs to the technical field of aircraft control, and in particular relates to an aircraft control system with network redundancy. Background technique
[0002] The basic function of the aircraft control system is to ensure the stable attitude of the aircraft through a certain control algorithm according to certain index requirements, and guide the aircraft to the desired position through a given control strategy to complete the established flight mission. At the same time, during the flight, the information exchange between the aircraft and the ground control station is realized.
[0003] At present, the aircraft control systems on the market are mainly aimed at the single-redundancy control of a single aircraft, which can better meet the installation and use requirements of small aircraft. However, for aircraft carrying high-cost reconnaissance / surveillance payloads, or even large and medium-sized aircraft that integrate reconnaissan...